NTSB CAROL · Event
Event WPR26LA064
Registry · N87PM
FAA Aircraft Registry record.
Make / Model
MOONEY M20J
Year of manufacture
1983 · 42 years old at event
Engine
LYCOMING AEIO-360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19830518
ADS-B equipped
Yes — Mode-S ABF54E
Registrant of record
MONA LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
On December 17, 2025, about 1230 Pacific standard time, a Mooney M20J, N87PM, was substantially damaged when it was involved in an accident near Silver Springs, Nevada. The pilot and passenger sustained serious injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. The pilot stated that the flight was a return trip from Lake Havasu City Airport (HII) to his home airport in Florence, Oregon (6S2). He had flown the route with his wife and dog on multiple previous occasions, and Silver Springs, Nevada (SPZ), was their usual intermediate stop. The pilot stated that he checked the weather that morning, and it indicated they had an opportunity to fly back that day, with a window of visual conditions at Florence remaining open until 1700. He did not check en route weather beyond reviewing winds aloft information. After takeoff from Lake Havasu, they climbed to 8,500 ft, and as they flew through the desert he observed numerous dust clouds on the surface. Skies were otherwise clear, and visual meteorological conditions prevailed. They discussed whether they should continue but decided that their dog needed a bathroom break and a walk, so they initiated a descent into Silver Springs. They encountered turbulence during the descent, but this was not particularly unusual based on his experience with desert operations. During the approach, the pilot heard nothing when he selected the automated weather observation system (AWOS) frequency. He reported that he could not see a windsock, so he decided to land on runway 6 because he understood it to be the “calm wind” runway. The wind was strong and gusting during the approach, and the pilot reported that the airplane touched down about midfield. Almost immediately, he decided to perform a go-around. He pulled back on the control yoke while pushing all the engine controls fully forward. The engine did not respond with the power he was accustomed to, and due to the strong turbulence, he was unable to observe the engine instruments. The airplane would not climb, and each time he pulled back on the control yoke the stall warning horn sounded. As the airplane approached the end of the runway, he began a left turn to avoid buildings, and the airplane settled into a field. The airplane struck a fence and tumbled, before it came to rest inverted about 2,500 ft northeast of the departure end of runway 6. A Notice to Airmen (NOTAM) current at the time of the accident indicated that the AWOS was out of service. The closest weather-reporting station, at Reno/Tahoe International Airport, located about 25 miles west of SPZ, indicated wind from 270° at 23 knots, gusting to 38 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2025_WPR26LA064.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall, go-around, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
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- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA)
Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint
Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Conference Paper
Prediction of stall and post-stall behavior of airfoils at low and high Reynolds numbers
An interactive boundary-layer method, together with the e(super n)-approach to the calculation of transition, has been used to predict the stall and post-stall behavior of airfoils at low and high Rey…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Low Level Turbulence Detection For Airports
Abstract—— Low level wind shear and turbulence present a serious safety risk to aircraft during the approach, landing and take-off phases.
- Embry-Riddle Scholarly Commons 2018 · Journal article (IJAAA)
Evaluating the Effect of Turbulence on Aircraft During Landing and Take-Off Phases
—— Low level wind shear and turbulence present a serious safety risk to aircraft during the approach, landing and take-off phases.
Browse the full corpus — academia portal ↗